CN105189033B - 机身结合方法及定位板 - Google Patents

机身结合方法及定位板 Download PDF

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Publication number
CN105189033B
CN105189033B CN201480016491.7A CN201480016491A CN105189033B CN 105189033 B CN105189033 B CN 105189033B CN 201480016491 A CN201480016491 A CN 201480016491A CN 105189033 B CN105189033 B CN 105189033B
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CN
China
Prior art keywords
positioning plate
trunk
fuselage
locator
pin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201480016491.7A
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English (en)
Chinese (zh)
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CN105189033A (zh
Inventor
柳原英康
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of CN105189033A publication Critical patent/CN105189033A/zh
Application granted granted Critical
Publication of CN105189033B publication Critical patent/CN105189033B/zh
Active legal-status Critical Current
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/10Aligning parts to be fitted together
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068Fuselage sections
    • B64C1/069Joining arrangements therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01Aircraft parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
CN201480016491.7A 2013-03-29 2014-03-17 机身结合方法及定位板 Active CN105189033B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2013-073092 2013-03-29
JP2013073092A JP6219055B2 (ja) 2013-03-29 2013-03-29 機体結合方法及びストロングバック
PCT/JP2014/057059 WO2014156745A1 (ja) 2013-03-29 2014-03-17 機体結合方法及びストロングバック

Publications (2)

Publication Number Publication Date
CN105189033A CN105189033A (zh) 2015-12-23
CN105189033B true CN105189033B (zh) 2019-03-08

Family

ID=51623726

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480016491.7A Active CN105189033B (zh) 2013-03-29 2014-03-17 机身结合方法及定位板

Country Status (6)

Country Link
EP (1) EP2979810B1 (ja)
JP (1) JP6219055B2 (ja)
CN (1) CN105189033B (ja)
BR (1) BR112015023903B1 (ja)
CA (1) CA2905255C (ja)
WO (1) WO2014156745A1 (ja)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
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US11131982B2 (en) * 2014-09-17 2021-09-28 The Boeing Company Fuselage manufacturing system
US11273930B2 (en) * 2014-09-17 2022-03-15 The Boeing Company Cradle system for shaping fuselage sections
US9682788B2 (en) 2014-09-17 2017-06-20 The Boeing Company Fuselage manufacturing system
JP6513584B2 (ja) * 2016-02-02 2019-05-15 三菱重工業株式会社 保持治具固定装置
JP6622645B2 (ja) 2016-04-20 2019-12-18 川崎重工業株式会社 航空機胴体組立治具およびその使用方法
CN107253531B (zh) * 2017-04-21 2019-11-15 陕西飞机工业(集团)有限公司 一种悬挂交点定位器的协调安装方法
US10723485B2 (en) * 2018-04-18 2020-07-28 The Boeing Company Apparatus that supports an aircraft fuselage without exterior surface contact
CN113460326B (zh) * 2021-06-25 2023-07-21 成都飞机工业(集团)有限责任公司 一种机身立式装配主定位框变形计算及辅助控制方法
FR3138121A1 (fr) * 2022-07-25 2024-01-26 Airbus Operations Plateforme d’assemblage destinée à manipuler au moins une coque inférieure d’aéronef sans la déformer en vue d’un assemblage d’un corps de fuselage d’aéronef.
EP4446696A1 (en) * 2023-04-13 2024-10-16 Airbus Operations GmbH Real-time determining of required characteristics for junction of hollow components during an alignment process

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES144849A1 (es) * 1937-03-13 1940-07-01 Messerschmitt Boelkow Blohm UN PROCEDIMIENTO Y DISPOSITIVO PARA LA FABRICACIoN EN SERIE DE PARTES DE AVIONES
FR852865A (fr) * 1938-04-09 1940-03-05 Messerschmitt Boelkow Blohm Procédé et dispositif pour la construction de pièces de grandes dimensions, composées d'éléments individuels et principalement des parties d'avions
DE677621C (de) * 1938-04-10 1939-06-29 Messerschmitt Boelkow Blohm Bauruestung zum Aufbau von Flugzeugruempfen, -tragflaechen u. dgl.
JPH0441496U (ja) * 1990-08-07 1992-04-08
RU2042918C1 (ru) * 1993-04-15 1995-08-27 Юрий Семенович Соломонов Способ сборки ступеней многоступенчатого летательного аппарата с секциями транспортно-пускового контейнера
FR2821778B1 (fr) * 2001-03-07 2004-11-19 S O C O A Soc De Conception Co Procede d'assemblage automatisee de structures volumineuses notamment aeronautiques, dispositifs et produit logiciel permettant de le mettre en oeuvre
JP4444033B2 (ja) * 2004-08-10 2010-03-31 三菱重工業株式会社 航空機の機体の製造方法
DE102004056284B4 (de) * 2004-11-22 2010-08-26 Airbus Deutschland Gmbh Vorrichtung zum Transport von Bauteilen für Verkehrsmittel
US7461711B2 (en) * 2004-11-24 2008-12-09 The Boeing Company Superconducting crawler system for a production line
US7624488B2 (en) * 2004-12-07 2009-12-01 The Boeing Company One-piece barrel assembly cart
US7756321B2 (en) * 2007-02-28 2010-07-13 The Boeing Company Method for fitting part assemblies
US8733707B2 (en) * 2008-04-17 2014-05-27 The Boeing Company Line transfer system for airplane
JP5112361B2 (ja) * 2009-02-27 2013-01-09 三菱重工業株式会社 航空機構造体製造装置
DE102009018991A1 (de) * 2009-05-01 2010-11-04 Airbus Operations Gmbh Vorrichtung zur räumlichen Ausrichtung von mindestens zwei Untergruppenbauteilen sowie Verfahren
DE102009034416B4 (de) * 2009-07-23 2011-06-30 Airbus Operations GmbH, 21129 Verfahren und Vorrichtung zur Systeminstallation sowie Frachtladesystem
JP5576650B2 (ja) * 2009-12-25 2014-08-20 川崎重工業株式会社 複合材料構造物製造用成形型
CN102249006A (zh) * 2011-05-11 2011-11-23 西安飞机工业(集团)有限责任公司 飞机总装配机身大部件移动对接装置
US9014836B2 (en) * 2011-12-15 2015-04-21 The Boeing Company Autonomous carrier system for moving aircraft structures

Also Published As

Publication number Publication date
EP2979810A4 (en) 2016-11-16
CA2905255C (en) 2018-02-20
WO2014156745A1 (ja) 2014-10-02
BR112015023903A2 (pt) 2017-07-18
CA2905255A1 (en) 2014-10-02
CN105189033A (zh) 2015-12-23
EP2979810A1 (en) 2016-02-03
BR112015023903B1 (pt) 2023-02-14
JP2014195855A (ja) 2014-10-16
JP6219055B2 (ja) 2017-10-25
EP2979810B1 (en) 2020-07-22

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